Home Nonlinear thermal radiation and the slip effect on a 3D bioconvection flow of the Casson nanofluid in a rotating frame via a homotopy analysis mechanism
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Nonlinear thermal radiation and the slip effect on a 3D bioconvection flow of the Casson nanofluid in a rotating frame via a homotopy analysis mechanism

  • Yijie Li , Mariam Imtiaz , Wasim Jamshed EMAIL logo , Sadique Rehman , Mohamed R. Eid , Nor Ain Azeany Mohd Nasir , Nur Aisyah Aminuddin , Assmaa Abd-Elmonem , Nesreen Sirelkhitam Elmki Abdalla , Rabha W. Ibrahim , Ayesha Amjad and Sayed M. El Din
Published/Copyright: December 31, 2023
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Abstract

This theoretical work suggests a novel nonlinear thermal radiation and an applied magnetic feature-based three-dimensional Casson nanomaterial flow. This flow is assumed in the rotating frame design. Gyrotactic microorganisms (GMs) are utilized in the Casson nanofluid to investigate bioconvection applications. The altered Buongiorno thermal nano-model is used to understand the thermophoretic and Brownian mechanisms. Convective boundary conditions must be overcome to solve the flow problem. With suitable variables, the dimensionless pattern of equations is obtained. The solutions to the nonlinear formulations are then obtained using semi-analytical simulations using a homotopy analysis mechanism. It was found that the velocity outline is enhanced with the enhancing estimations of the buoyancy ratio, rotation factor, and Casson parameter while it is reduced with mixed convection, porosity, slippery parameters, and Rayleigh number. The temperature profile is increased with radiation, the temperature ratio, the thermophoretic parameter, the Brownian parameter, and the Biot number. The Brownian parameter reasons an improvement in the concentration outline contrary to the thermophoretic parameter. The concentration of GMs is decreased with the Peclet number inversely to the Lewis number effect, which causes an increase in the microorganisms’ concentration.

Nomenclature

u , v , w

velocity components

Ω

dimensional rotational parameter

ρ m

density of the microorganism

T w , C w

surface temperature and concentration

T , C

surrounding temperature and concentration

C p

specific heat at constant pressure

σ

electrical conductivity

ρ

density of the fluid

k f

thermal conductivity of the nanofluid

μ f

dynamic viscosity of the nanofluid

β

Casson parameter

D B

Brownian diffusion coefficient

D T

thermophoretic coefficient

k *

Porosity parameter

K 1

dimensional slip parameter

h f

convective heat transfer coefficient

Pe

Peclet number

A

slip parameter

δ 1

concentration difference parameter of microorganisms

Bi

Biot number

ω

rotation parameter

N b

Brownian motion parameter

N t

thermophoretic parameter

Sc

Schmidt number

R d

radiation parameter

λ

mixed convection parameter

M

magnetic parameter

N c

Rayleigh number

N r

buoyancy ratio parameter

θ w

temperature ratio parameter

Pr

Prandtl number

Le

Lewis number

1 Introduction

Nanofluids (NFs) are a type of heat transfer fluids that consist of a base fluid and small particles, typically ranging from 1 to 100 nm in size, which are suspended within the fluid. These particles are usually prepared by materials such as metals, metal oxides, or carbon nanotubes. NFs have been shown to have several applications in various industries, including heat transfer (see a review by Panduro et al. [1]), where NFs have significantly higher thermal conductivity than their base fluids [2], making them useful for applications where high heat transfer rates are required [3], such as in cooling systems for electronics, engines, and power plants [4,5]. Solar energy is another application where NFs can be utilized to develop the efficiency of solar thermal collectors by increasing the heat transfer from the collector to the fluid, thereby improving the overall energy conversion efficiency (see a review work of Shah and Ali [6]). Biomedical engineering is the recent application of NFs, where NFs have potential applications in drug delivery [7] and hyperthermia cancer therapy [8], where they can be used to target specific cells or tissues. Environmental remediation includes the application of NFs, whenever NFs can be used to remove contaminants from soil and groundwater by enhancing the rate of chemical reactions or physical processes such as adsorption (see Sonawane et al. [9] and Alsaady et al. [10] for an advanced study). Lubrication NFs can be used as lubricants in various industrial applications, including aerospace and automotive industries, due to their ability to reduce friction and wear [11]. Electronic cooling in NFs can be used as coolants in electronics to improve their heat dissipation efficiency, leading to longer lifetimes and increased performance [12]. Overall, NFs have the potential to revolutionize various industries by offering improved heat transfer and other properties compared to traditional fluids. Khan et al. [13] proposed the mechanical aspects of Maxwell NF flow in a dynamic system with entropy generation. However, further research is needed to fully understand their behavior and optimize their performance in specific applications.

The Casson NF model (CNFM) is a rheological model that describes the behavior of fluids with a yield stress, such as NFs. NFs are suspensions of nanoparticles in a base fluid, typically water or oil, and have unique thermal and rheological properties compared to their base fluids [14]. Vasefi et al. [15] studied the turbulent forced convective heat transport of CuO/water NF flow using an artificial intelligence network in a square duct. Gul et al. [16] scrutinized the simulation of water-based hybrid NF flow over a porous cavity with heat transfer. The solution to the flow problem is acquired numerically through the control volume method.

The CNFM assumes that the fluid behaves as a Bingham plastic, which means that it has a yield stress below which it does not flow, and above which it behaves like a Newtonian fluid with a constant viscosity [17, 18]. For NFs, the CNFM can be modified to include the effects of the concentration and size of nanoparticles. The viscosity and yield stress of NFs typically increase with increasing nanoparticle concentration, while the size of the nanoparticles can affect the yield stress but has little effect on the viscosity [19]. The CNFM is commonly used to predict the rheological properties of NFs and to optimize their use in various applications, such as heat transfer and liquid flowing in a microchannel [20,21]. However, it should be noted that the model has limitations, and more complex models may be required for accurately predicting the behavior of NFs under certain conditions [22,23].

Gyrotactic microorganisms (GMs) are microorganisms that have the ability to orient themselves in the direction of gravity. They are able to sense gravity and use it to move up or down in a fluid environment. Gyrotaxis is the process by which these microorganisms orient themselves with respect to the gravitational field. GMs can be found in a variety of aquatic environments, including oceans, lakes, and rivers. Examples of GMs include certain types of plankton, algae, and bacteria (see Hosseinzadeh et al. [24]). The ability of GMs to move in response to gravity has important ecological implications [25]. For example, in aquatic environments with vertical gradients in nutrient and light availability [26], gyrotaxis allows these microorganisms to position themselves under optimal conditions for growth and survival [27]. In addition, gyrotaxis can also affect the vertical distribution of microorganisms in aquatic ecosystems, with implications for nutrient cycling and carbon sequestration [28]. The study of GMs has applications in fields such as ecology, environmental science, and microbiology. It can also have practical applications in areas such as bioremediation, where GMs can be used to remove contaminants from water or soil [29]. Zuhra et al. [30] proposed the simulations of bioconvection second-grade NF flow with the suspension of nanoparticles containing GMs. For simulation, the optimal homotopy analysis method is utilized to evaluate the flow problem. Majeed et al. [31] explored the 2D bioconvection magnetized Casson nanoliquid flowing with Brownian and thermophoretic phenomena containing GMs. The thermal examination of a radiative bioconvective magnetized flow including GMs with the energy of activation was shown by Majeed et al. [32]. Zeeshan et al. [33] scrutinized the semi-analytical method with the DTM-Pade approach in a squeezing flow between two circular plates.

3D rotating geometry (3D-RG) refers to the study and manipulation of three-dimensional shapes and objects as they rotate around an axis or pivot point. This concept is commonly used in fields such as computer graphics, animation, and engineering. In computer graphics and animation, 3D-RG is often used to create realistic-looking objects and scenes. By applying mathematical formulas and algorithms to 3D models, it is possible to simulate the way an object would move and rotate in real life. This is used to create dynamic visual effects such as spinning logos, rotating planets, and flying objects. In engineering, 3D-RG is used to design and analyze complex structures such as gears, turbines, and engines. By modeling these structures in 3D and simulating their rotation, engineers can test their performance under different conditions and identify potential problems before building a physical prototype. Overall, 3D-RG is a powerful tool for visualizing and manipulating three-dimensional objects and structures, and it has a wide range of practical implementations in various disciplines. When a 3D object rotates in a fluid, it creates a disturbance in the fluid flow around it [34]. The fluid will experience forces due to the rotation of the object, which can cause the fluid to move in different ways. This phenomenon is known as fluid–structure interaction. The behavior of the fluid around the rotating object depends on diverse considerations, such as the speed of rotation, the size and shape of the object, the viscosity of the fluid, and the properties of the fluid itself [35]. One example of 3D-RG in a fluid is a propeller in water. As the propeller blades rotate, they create a flow of water around them. This flow of water produces forces that propel the boat forward (see Juhany et al. [36]). The design of the propeller blades is crucial for optimizing the efficiency of this process. Another example is a wind turbine. As the blades of the turbine rotate, they interact with the air around them, creating a flow of air that generates electricity [37]. In summary, when 3D-RG interacts with a fluid, it creates disturbances in the fluid flow around it, which can cause the fluid to move in different ways. The behavior of the fluid depends on various factors, and understanding these factors is crucial for optimizing the performance of rotating machinery in fluid environments.

Thermal radiative fluxing is the emission of electromagnetic waves by matter that is at a temperature higher than absolute zero. The rate at which thermal radiation is emitted depends on the temperature of the emitting object and the emissivity of the material. In NFs, the nanoparticles can increase the emissivity of the fluid, which leads to a higher rate of thermal radiation emission (TRE) [38,39]. The increased TRE in NFs can have several effects on the thermal properties of the fluid. For example, it can improve the heat transference rate between the fluid and a heat source or sink. It can also influence the temperature distribution within the fluid, which can impact the fluid flow behavior [40]. However, the exact mechanisms by which TRE affects the thermal properties of NFs are still being studied. Some studies have suggested that the size, shape, and concentricity of the nanoparticles can affect the emissivity of the fluid and therefore the rate of TRE [41]. Other studies have examined the impact of TRE on the thermal conductivity of the fluid, which can also be influenced by the nanoparticle properties [42,43]. In summary, thermal radiation is an important factor in the thermal properties of NFs [44]. Its effects can lead to enhanced heat transfer and fluid behavior; however, much research is needed to fully understand the mechanisms involved.

The homotopy analysis methodology (HAM) is a great analytical procedure used in the study of nonlinear problems in various fields, including fluid mechanics. It was first introduced by J.H. He in 1999 and has since been widely used in many scientific and engineering applications. In fluid mechanics, the HAM can be directed to solve a broad collection of challenges, including laminar and turbulent flow (see Ige et al. [45]), boundary layer flow, and free surface flow. The method involves constructing a homotopy between a known linear solution and the nonlinear solution of interest [46]. This allows the nonlinearity of the problem to be gradually introduced and solved systematically [47]. The HAM can also be used to study the stability of fluid flows, as well as the bifurcation behavior of fluid systems. It has been successfully applied to investigate complex phenomena such as chaos and turbulence in fluid mechanics [48]. One of the main advantages of the HAM is its ability to provide closed-form solutions for nonlinear problems that are difficult or impossible to solve using traditional analytical methods [49]. Khan et al. [50] investigated the thin film flow of a second-grade fluid past a stretching sheet with heat transfer in a porous medium. The solution of the model is acquired using the HAM. Ahmad et al. [51] studied the MHD thin film flow of the Oldroyd-B fluid with bioconvection phenomenon and activation energy using the HAM. This makes it a useful tool for researchers and engineers working in fluid mechanics and related fields. Generally, the HAM is a promising approach for the study of nonlinear problems in fluid mechanics, and its potential for solving complex problems and providing valuable insights into fluid behavior makes it an important tool for researchers and engineers in this field.

The previous theoretical investigations point to a previously non-explored nonlinear thermal radiation and the applied magnetic feature-based three-dimensional Casson nanomaterial flow in porous media. In the design of the rotating frame, the flow has been assumed. Bioconvection flows are intimately connected to mechanical and real-life phenomena, such as the construction and design of biological cells, biological conjugates, and microscopic biological systems, and they have emerged as a hot issue in present-day scientific research because of this close relationship. To research the applications of bioconvection, GMs are used in the Casson NF. In order to include the thermophoretic and Brownian phenomena, the Buongiorno thermal nano-model has been modified. In order to resolve the flow issue, convective boundary conditions have to be circumvented. It is possible to generate the dimensionless pattern of equations if appropriate variables are used. Subsequently, the answers to the nonlinear formulations are derived by the use of an analytical technique called the homotopy analysis mechanism (HAM).

2 Mathematical formulation

This article centers on a 3-D Casson NF investigation containing rotating GMs. A cartesian system places the surface in the xy -plane and the fluid in area z 0 . An elastic sheet is stretched with an angular velocity Ω along the x-axis, as shown in Figure 1. The initiation energy relatives and nonlinear thermal pattern are taken into consideration in the energy and concentration equations, respectively. In a velocity field, u and v stand for the normal and horizontal velocity components, respectively. Using these flow possessions, the main equations for the Casson NF with motile microbes are demarcated as tracks [52,53]. In this article, the following presumptions are made:

  1. The velocity components along the x, y, and z directions are u , v and w separately.

  2. The coordinate system is assumed in such a way that z-axis is supposed to be orthogonal to the sheet, whereas the x- and y -axis are chosen sideways with the plate. Continuous distortion of the plate is measured along the x- and y -axis with velocities u w ( x ) and v w ( y ) , respectively.

  3. Because the flow is generated by a bilinear stretched surface, the pressure gradient along the sheet is ignored.

  4. While viscous dissipation is taken into account, velocity slippery with a dimensional slippery factor K 1 and non-linear thermal radiation are not taken into consideration.

  5. The Buongiorno thermal nano-model is used with the suspension of GMs.

  6. The NF flow is incompressible and steady in a rotating system.

(1) u x + v y + w z = 0 ,

(2) u u x + v u y + w u z 2 Ω v = ν 1 + 1 β z u z σ ρ f B 0 2 u ν k * u + 1 ρ f [ ( 1 C ) ρ f g β g ( T T ) ( ρ p ρ f ) g ( C C ) ( n n ) g γ ( ρ m ρ f ) ] ,

(3) u v x + v v y + w v z + 2 Ω u = ν 1 + 1 β z v z σ ρ f B 0 2 v ν k * v ,

(4) u T x + v T y + w T z = α m + 16 σ * T 3 3 ( ρ c ) f k * 2 T z 2 + ( ρ c ) p ( ρ c ) f D B C z T z + D T T T z 2 ,

(5) u C x + v C y + w C z = D B 2 C z 2 + D T T 2 T z 2 ,

(6) u n x + v n y + w n z + b W c ( C w C ) z n n z = D m 2 n z 2 .

Figure 1 
               Flow geometry of the problem.
Figure 1

Flow geometry of the problem.

The justified boundary conditions for the current analysis are

(7) u = u w ( x ) + K 1 1 + 1 β u y , v w ( y ) = by , k f T y = h f ( T w T ) , D B C y + D T T T y = 0 , n = n w at z = 0 , u 0 , v 0 , T T , C C , n n as z ,

where β is the Casson parameter, ν is the kinematics viscosity, ρ f is the density of the NFs, k * is the porosity parameter, g is the gravitational acceleration, Ω denotes the dimensional rotational parameter, β g is the volume expansion coefficient, ρ p is the density of the nanoparticles, ρ m is the density of the microorganism, T is the temperature, T w and T , respectively, represent the surface and surrounding temperatures, C w and C , respectively, represent the surface and surrounding concentrations, α m = k ( ρ c ) f is the thermal diffusivity (with k being the thermal conductivity), ( ρ c ) f is the heat capacity of the fluid, ( ρ c ) p is the heat capacity of the nanoparticles, h f represents the convective heat transfer coefficient, K 1 denotes the dimensional slip parameter, D B stands for the Brownian diffusion coefficient, and D T is the thermophoretic coefficient.

3 Method of solution

To simplify the flow governing equations and the associated boundary conditions, we introduce the following similarity transformations:

(8) u = ax f ( η ) , v = byg ( η ) , w = a ν ( f ( η ) + g ( η ) ) , η = a ν z , θ ( η ) = T T T w T , ϕ ( η ) = C C C w C , χ ( η ) = n n n w n .

It is evident that the similarity variables described in equation (8) satisfy equation (1) in the same way. Now, one can obtain this by applying equation (8) to equations (2)–(7):

(9) 1 + 1 β f + ( f + g ) f f 2 + 2 ω g ( M + K ) f + λ ( θ N r ϕ N c χ ) = 0 ,

(10) 1 + 1 β g + ( f + g ) g f g 2 ω f ( M + K ) g = 0 ,

(11) 1 + 4 3 R d ( 1 + ( θ w 1 ) θ ) 3 θ + R d [ 3 ( θ w 1 ) ( θ ) 2 ] [ 1 + ( θ w 1 ) θ ] 2 + Pr [ ( f + g ) θ + N b θ ϕ + N t θ 2 ] = 0 ,

(12) ϕ + Sc ( f + g ) ϕ + N t N b θ = 0 ,

(13) χ + Le ( f + g ) χ Pe [ ϕ ( χ + δ 1 ) + χ ϕ ] = 0 .

The transformed boundary conditions are

(14) f ( 0 ) = g ( 0 ) = 1 , f ( 0 ) = 1 + A 1 + 1 β f , θ ( 0 ) = Bi ( θ ( 0 ) 1 ) , Nb ϕ ( 0 ) + Nt θ ( 0 ) = 0 , χ ( 0 ) = 1 . f ( ) 0 , g ( ) 0 , θ ( ) 0 , ϕ ( ) 0 , χ ( ) 0 .

The parameters are the rotation parameter ω = Ω a , the mixed convection parameter λ = β g g T ( 1 C ) a u w , the magnetic parameter M = σ B 0 2 a ρ f , the Rayleigh number N c = γ g T ( ρ m ρ f ) ( n w n ) β g ρ f ( 1 C ) T , the buoyancy ratio parameter N r = ( ρ p ρ f ) ( C w C ) β g ρ f ( 1 C ) T , the radiation parameter R d , the temperature ratio parameter θ w = T w T , θ w > 1 , the Prandtl number Pr , the Brownian constant N b = D B τ ( C w C ) ν , the thermophoresis parameter N t = D T τ ( T w C ) ν T , the Schmidt number Sc = ν D B , the Peclet number Pe = b w m D m , the concentration difference constant of the microorganism δ 1 = n n w n , and the Lewis number Le = ν D m . Bi denotes the Biot number, and the slip parameter A = N 0 a ν . The skin friction coefficient C f and the local Nusselt number N u x , which are both physical variables of relevance, are defined as

(15) C f = τ w ρ f U w 2 , N u x = x q w k ( T w T ) , S h x = x q s D B ( C w C ) , N n = x q n D n ( n w n ) .

The surface shear stress τ w , the surface heat flow q w , the wall mass flux q s , and wall motile microorganisms’ flux N n are determined as

(16) τ w = μ f 1 + 1 β u z , q w = k T z , q s = D B C z , q n = D m n z at z = 0 .

By employing the similarity transformation (8), we obtain

(17) ( Re x ) 1 / 2 C f x = 1 + 1 β f ( 0 ) , ( Re x ) 1 / 2 N u x = 1 + 4 3 R d ( ( θ w 1 ) θ ( 0 ) + 1 ) 3 θ ( 0 ) , ( Re x ) 1 2 S h x = ϕ ( 0 ) , ( Re x ) 1 2 N n = χ ( 0 ) ,

where Re x = a x 2 ν f is the local Reynolds number.

4 HAM

Liao first proposed the homotopy strategy in 1992. The homotopic technique is preferred to find nonlinear model solutions. In contrast to prior perturbations and non-perturbative processes, the homotopy assessment approach enables us to quickly adjust and alter the convergence position and charges of learned guesses in response to changing circumstances. This is the case because it gives us the ability to examine homotopy. In a nutshell, the homotopy evaluation has the following additional advantages: it can be used to precisely make assumptions about a nonlinear mathematical challenge by choosing particular units of base functions; it is valid even if a given nonlinear problem does not contains either small or extensive parameters at all; and it can provide us with a convenient way to change and manipulate the convergence place and charge of estimation collection when it is necessary to do so.

4.1 Limitations of HAM

In the field of mathematics, HAM is a sophisticated approach that is used to solve nonlinear differential equations. On the other hand, just like any other approach, it does have certain drawbacks. HAM has several significant drawbacks, and some of which are listed as follows:

1) Convergence: The convergence of the HAM series solution is not guaranteed for all types of problems. In some cases, the series may not converge or may converge very slowly, leading to inaccurate or impractical results. The convergence behavior depends on the nature of the problem and the chosen auxiliary linear operator.

2) Solution dependence: The HAM solution is highly dependent on the initial approximation and the auxiliary linear operator. Different choices of these parameters can lead to different results. It can be challenging to determine the optimal values, and there is no systematic procedure for selecting them.

3) Computational complexity: The computational complexity of the HAM can be high, especially for problems with multiple nonlinear terms. The process of calculating the coefficients of the series solution can be time-consuming and require substantial computational resources.

4) Singularity problems: HAM may encounter difficulties when dealing with singularities, such as poles or essential singularities, in the domain of the problem. The presence of singularities can affect the convergence behavior of the series solution and require special treatment.

5) Limited applicability: HAM is primarily suitable for solving differential equations with small parameters or perturbation terms. It may not be as effective for problems with large nonlinearities or strong nonlinearity.

6) Lack of rigorous error analysis: HAM lacks a rigorous error estimation or error control mechanism. It can be challenging to assess the accuracy or reliability of the obtained solutions.

7) Limited extension to higher dimensions: While HAM has been successfully applied to one-dimensional problems, its extension to higher-dimensional problems is more challenging. The complexity and computational requirements increase significantly in higher dimensions.

Despite these limitations, the HAM remains a valuable tool for solving a wide range of nonlinear problems. Researchers continue to develop new variants and improvements to address some of these limitations and enhance the applicability of the method. Figure 2 shows the phases of the homotopic approach [54].

Figure 2 
                  Methods for obtaining numerical results.
Figure 2

Methods for obtaining numerical results.

By using the HAM in Mathematica 13, an analytical solution to the higher-order ordinary differential equations may be obtained. The following are some definitions for the initial estimates and linear operators:

(18) f 0 ( η ) = 1 1 + A 1 + 1 β ( 1 e η ) , g 0 ( η ) = e η , θ 0 ( η ) = Bi 1 + Bi e η , ϕ 0 ( η ) = NtBi Nb ( 1 + Bi ) e η , χ 0 ( η ) = e η .

(19) L f = f f , L g = g g , L θ = θ θ , L ϕ = ϕ ϕ , L χ = χ χ ,

with

(20) L f [ C 1 + C 2 exp ( η ) + C 3 exp ( η ) ] = 0 , L g [ C 4 exp ( η ) + C 5 exp ( η ) ] = 0 , L θ [ C 6 exp ( η ) + C 7 exp ( η ) ] = 0 , L ϕ [ C 8 exp ( η ) + C 9 exp ( η ) ] = 0 , L χ [ C 10 exp ( η ) + C 11 exp ( η ) ] = 0 ,

where C i ( i = 1 11 ) are arbitrary constants.

4.2 Zeroth order

The following expressions represent the zero-order deformation for the typical current NFs:

(21) ( 1 q ) L f [ f ( η , q ) f 0 ( η ) ] = q h f N f [ f ( η , q ) , g ( η , q ) , θ ( η , q ) , ϕ ( η , q ) , χ ( η , q ) ] ,

(22) ( 1 q ) L g [ g ( η , q ) g 0 ( η ) ] = q h g N g [ f ( η , q ) , g ( η , q ) ] ,

(23) ( 1 q ) L θ [ θ ( η , q ) θ 0 ( η ) ] = q h θ N θ [ f ( η , q ) , θ ( η , q ) , ϕ ( η , q ) ] ,

(24) ( 1 q ) L ϕ [ ϕ ( η , q ) ϕ 0 ( η ) ] = q h ϕ N ϕ [ f ( η , q ) , θ ( η , q ) , ϕ ( η , q ) ] ,

(25) ( 1 q ) L χ [ χ ( η , q ) χ 0 ( η ) ] = q h χ N χ [ f ( η , q ) , ϕ ( η , q ) , χ ( η , q ) ] .

In the present case, N f , N g , N θ , N ϕ , and N χ are the nonlinear operators and are given as

(26) N f [ f ( η , q ) , g ( η , q ) , θ ( η , q ) , ϕ ( η , q ) , χ ( η , q ) ] = 1 + 1 β 3 f ( η , q ) η 3 + ( f ( η , q ) + g ( η , q ) ) 2 f ( η , q ) η 2 f ( η , q ) η 2 + 2 ω g ( η , q ) [ M + K ] f ( η , q ) η + λ ( θ ( η , q ) N r ϕ ( η , q ) N c χ ( η , q ) ) ,

(27) N g [ f ( η , q ) , g ( η , q ) ] = 1 + 1 β 2 g ( η , q ) η 2 + ( f ( η , q ) + g ( η , q ) ) g ( η , q ) η 2 g ( η , q ) f ( η , q ) η 2 2 ω f ( η , q ) η [ M + K ] g ( η , q ) ,

(28) N θ [ f ( η , q ) , θ ( η , q ) ] = 1 + 4 3 R d ( 1 + ( θ w 1 ) θ ) 3 2 θ ( η , q ) η 2 + R d 3 ( θ w 1 ) θ ( η , q ) η 2 [ 1 + ( θ w 1 ) θ ( η , q ) ] 2 + Pr f ( η , q ) θ ( η , q ) η + g ( η , q ) θ ( η , q ) η + N b θ ( η , q ) η ϕ ( η , q ) η + N t θ ( η , q ) η 2 ,

(29) N ϕ [ f ( η , q ) , θ ( η , q ) , ϕ ( η , q ) ] = 2 ϕ ( η , q ) η 2 + Sc ( f ( η , q ) ϕ ( η , q ) η + g ( η , q ) ϕ ( η , q ) η ) + N t N b 2 θ ( η , q ) η 2 ,

(30) N χ [ f ( η , q ) , ϕ ( η , q ) , χ ( η , q ) ] = 2 χ ( η , q ) η 2 + Le ( f ( η , q ) χ ( η , q ) η + g ( η , q ) χ ( η , q ) η ) Pe 2 ϕ ( η , q ) η 2 χ ( η , q ) + δ 1 2 ϕ ( η , q ) η 2 + χ ( η , q ) η ϕ ( η , q ) η ,

(31) f ( 0 , q ) = 0 , f ( 0 , q ) = 1 + A 1 + 1 β f ( 0 , q ) , f ( , q ) = 0 ,

(32) g ( 0 , q ) = 1 , g ( , q ) = 0 ,

(33) θ ( 0 , q ) = Bi ( θ ( 0 , q ) 1 ) θ ( , q ) = 0 .

(34) Nb ϕ ( 0 , q ) + Nt θ ( 0 , q ) = 0 .

(35) χ ( 0 , q ) = 1 , χ ( , q ) = 0 .

For q = 0 and q = 1 , (21)–(25) become

(36) q = 0 f ( η , 0 ) = f 0 ( η ) , and q = 1 f ( η , 1 ) = f ( η ) ,

(37) q = 0 g ( η , 0 ) = g 0 ( η ) , and q = 1 g ( η , 1 ) = g ( η ) ,

(38) q = 0 θ ( η , 0 ) = θ 0 ( η ) , and q = 1 θ ( η , 1 ) = θ ( η ) ,

(39) q = 0 ϕ ( η , 0 ) = ϕ 0 ( η ) , and q = 1 ϕ ( η , 1 ) = ϕ ( η ) ,

(40) q = 0 χ ( η , 0 ) = χ 0 ( η ) , and q = 1 χ ( η , 1 ) = χ ( η ) .

The Taylor expansion is used on (27) and (28), and we obtain

(41) f ( η , q ) = f 0 ( η ) + m = 1 f m ( η ) q m , f m ( η ) = 1 m ! m f ( η , q ) η m | q = 0 ,

(42) g ( η , q ) = g 0 ( η ) + m = 1 g m ( η ) q m , g m ( η ) = 1 m ! m g ( η , q ) η m | q = 0 ,

(43) θ ( η , q ) = θ 0 ( η ) + m = 1 θ m ( η ) q m , θ m ( η ) = 1 m ! m θ ( η , q ) η m | q = 0 ,

(44) ϕ ( η , q ) = ϕ 0 ( η ) + m = 1 ϕ m ( η ) q m , ϕ m ( η ) = 1 m ! m ϕ ( η , q ) η m | q = 0 ,

(45) χ ( η , q ) = χ 0 ( η ) + m = 1 χ m ( η ) q m , χ m ( η ) = 1 m ! m χ ( η , q ) η m | q = 0 .

By taking q = 1 in (29) and (30), the convergence of the series is found as

(46) f ( η ) = f 0 ( η ) + m = 1 f m ( η ) ,

(47) g ( η ) = g 0 ( η ) + m = 1 g m ( η ) ,

(48) θ ( η ) = θ 0 ( η ) + m = 1 θ m ( η ) ,

(49) ϕ ( η ) = ϕ 0 ( η ) + m = 1 ϕ m ( η ) ,

(50) χ ( η ) = χ 0 ( η ) + m = 1 χ m ( η ) .

4.3 m th -order

Now, we may explain the situation by referring to the mth distortion, which is as follows:

(51) L f [ f m ( η ) η m f m 1 ( η ) ] = h f R m f m ( η ) ,

(52) L g [ g m ( η ) η m g m 1 ( η ) ] = h g R m g m ( η ) ,

(53) L θ [ θ m ( η ) η m θ m 1 ( η ) ] = h θ R m θ m ( η ) ,

(54) L ϕ [ ϕ m ( η ) η m ϕ m 1 ( η ) ] = h ϕ R m ϕ m ( η ) ,

(55) L χ [ χ m ( η ) η m χ m 1 ( η ) ] = h χ R m χ m ( η ) ,

(56) f m ( 0 ) = 0 , f m ( ) = 0 ,

(57) g m ( 0 ) = 0 , g m ( ) = 0 ,

(58) θ m ( 0 ) = 0 , θ m ( ) = 0 ,

(59) ϕ m ( 0 ) = 0 , ϕ m ( ) = 0 ,

(60) χ m ( 0 ) = 0 , χ m ( ) = 0 .

The R m f ( η ) , R m g ( η ) , R m θ ( η ) , R m ϕ ( η ) and R m χ ( η ) are defined as follows:

(61) R m f ( η ) = 1 + 1 β f m 1 + k = 0 m 1 f m 1 k f k '' + k = 0 m 1 g m 1 k f k '' k = 0 m 1 f m 1 k f k + 2 ω g m 1 ( M + K ) f m 1 + λ ( θ m 1 N r ϕ m 1 N c χ m 1 ) ,

(62) R m g ( η ) = 1 + 1 β g m 1 '' + k = 0 m 1 f m 1 k g k + k = 0 m 1 g m 1 k g k k = 0 m 1 f m 1 k g k 2 ω f m 1 ( M + K ) g m 1 ,

(63) R m θ ( η ) = 1 + 4 3 R d ( 1 + ( θ w 1 ) θ m 1 ) 3 θ m 1 '' + R d 3 ( θ w 1 ) k = 0 m 1 θ m 1 k θ k 1 + ( θ w 1 ) k = 0 m 1 θ m 1 k θ k + Pr k = 0 m 1 f m 1 k θ k + k = 0 m 1 g m 1 k θ k + N b k = 0 m 1 ϕ m 1 k θ k + N t k = 0 m 1 θ m 1 k θ k ,

(64) R m ϕ ( η ) = ϕ m 1 '' + Sc k = 0 m 1 f m 1 k ϕ k + Sc k = 0 m 1 g m 1 k ϕ k + Nt Nb θ m 1 '' ,

(65) R m χ ( η ) = χ m 1 '' + Le k = 0 m 1 f m 1 k χ k + k = 0 m 1 g m 1 k χ k Pe k = 0 m 1 ϕ m 1 k '' χ k + δ 1 ϕ m 1 '' + k = 0 m 1 ϕ m 1 k χ k .

Utilizing specific solutions allows for the completion of the overarching solution, which is as follows:

(66) f m ( η ) = f m * ( η ) + C 1 + C 2 exp ( η ) + C 3 exp ( η ) ,

(67) g m ( η ) = g m * ( η ) + C 4 exp ( η ) + C 5 exp ( η ) ,

(68) θ m ( η ) = θ m * ( η ) + C 6 exp ( η ) + C 7 exp ( η ) ,

(69) ϕ m ( η ) = ϕ m * ( η ) + C 8 exp ( η ) + C 9 exp ( η ) ,

(70) χ m ( η ) = χ m * ( η ) + C 10 exp ( η ) + C 11 exp ( η ) .

5 Results and discussion

The influence of mixed convective factor λ on f' ( η ) is shown in Figure 3. It was found that the augmentation of λ drops the primary velocity profile. Figure 4 is plotted for different values of the buoyancy ratio variable N r on the primary velocity distribution. The rapidity increases, as the increase of N r promotes NF flow significantly. The influence of Rayleigh’s number N c on the primary rapidity profile is analyzed in Figure 5. It is shown that the rapidity of the liquid decreases as the value of N c increases. First, the buoyancy force increases when N c increases. Second, a destabilizing effect is generated owing to the existence of microorganisms that move vertically over the plate. As a consequence, the velocity profile drops along the increase of N c . Figures 6 shows the decrement of rapidity occurs as the value of porosity variable K rises. The existence of holes over the medium attracts the fluid flow towards the plate. Therefore, more drag force or resistance is produced on the plate, which resists the motion of the fluid. As shown in Figure 7, the value of Casson parameter β is directly related to rapidity of fluid. As β soars, the velocity of the fluid also augments. Figure 8 illustrates the change in the velocity slip A on the rapidity outline. It can be deduced that as A increases, the rapidity of liquid decreases. In this situation, the existence of rapidity slippage over the slab prevents the motion of fluid because the slip functions as a repellent, thus shrinking the thickness of the momentum boundary layer. As shown in Figure 9, as the rotation factor ω increases, it increases the primary velocity. A supplementary momentum is incorporated into the boundary layer along the increase of ω , which immensely acts on the acceleration of the flow. As illustrated in Figures 10, the enlargement of Casson parameter β drops the secondary velocity and its momentum boundary layer. The surge in β elevates the plastic dynamic viscosity that leads to the magnification of viscosity of the liquid. This phenomenon generates interference to the flow and eventually slows down the movement of fluid. The effect of porosity parameter K to secondary velocity is the same as its influence on the primary velocity. As in Figure 11, K promotes disturbance to the flow, thus lessening the thickness of the momentum boundary layer. The porosity parameter, as previously elucidated, serves to define the proportion of empty space within a medium that permits the passage of fluid. The aforementioned parameter plays a crucial role in shaping the dynamics of fluid flow within porous media. The present study aims to investigate the impact of variations in porosity on the streamlines pertaining to the second velocity profile. The discourse brings attention to a notable discovery: the amplification of streamlines resulting from the modification of the porosity parameter, particularly in relation to the second velocity profile which is illustrated in Figure 11. The observed improvement can be attributed to the interplay among porosity, velocity distribution, and fluid flow. The augmentation of porosity frequently results in the establishment of a more intricate network of conduits, facilitating the movement of fluid. Within the framework of the second profile of velocity, this phenomenon has the potential to yield a more seamless and efficient flow pattern. Increased porosity can enhance fluid flow by enabling smoother and more efficient movement, thereby leading to improved streamlines in the velocity profile.

Figure 3 
               Assessment of 
                     
                        
                        
                           λ
                        
                        \lambda 
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 3

Assessment of λ on f' ( η ) .

Figure 4 
               Assessment of 
                     
                        
                        
                           
                              
                                 N
                              
                              
                                 r
                              
                           
                        
                        {N}_{{\rm{r}}}
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 4

Assessment of N r on f' ( η ) .

Figure 5 
               Assessment of 
                     
                        
                        
                           
                              
                                 N
                              
                              
                                 c
                              
                           
                        
                        {N}_{{\rm{c}}}
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 5

Assessment of N c on f' ( η ) .

Figure 6 
               Assessment of 
                     
                        
                        
                           K
                        
                        K
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 6

Assessment of K on f' ( η ) .

Figure 7 
               Assessment of 
                     
                        
                        
                           β
                        
                        \beta 
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 7

Assessment of β on f' ( η ) .

Figure 8 
               Assessment of 
                     
                        
                        
                           A
                        
                        A
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 8

Assessment of A on f' ( η ) .

Figure 9 
               Assessment of 
                     
                        
                        
                           ω
                        
                        \omega 
                     
                   on 
                     
                        
                        
                           f'
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        {f\text{'}}(\eta )
                     
                  .
Figure 9

Assessment of ω on f' ( η ) .

Figure 10 
               Assessment of 
                     
                        
                        
                           β
                        
                        \beta 
                     
                   on 
                     
                        
                        
                           g
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        g(\eta )
                     
                  .
Figure 10

Assessment of β on g ( η ) .

Figure 11 
               Assessment of 
                     
                        
                        
                           K
                        
                        K
                     
                   on 
                     
                        
                        
                           g
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        g(\eta )
                     
                  .
Figure 11

Assessment of K on g ( η ) .

The impression of rotation factor ω on the secondary rapidity profile is shown in Figure 12. The proliferation of ω decreases the momentum of the liquid. The development of obstruction is directly proportional to the value of ω . Therefore, high ω means high constriction, which prevents the fluid from moving, resulting in the decrease of the velocity. Radiation is directly proportional to particles energy, and this can be proven by the graph’s trend in Figure 13, where the growth of radiation intensifies the temperature. The radiation that is emitted provides heat to the fluid continuously, leading to the escalation of molecules kinetic energy that boosts the collision among them, which ultimately improves the conductivity of the fluid. Hence, high radiation widens the thermal boundary layer thickness.

Figure 12 
               Assessment of 
                     
                        
                        
                           ω
                        
                        \omega 
                     
                   on 
                     
                        
                        
                           g
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        g(\eta )
                     
                  .
Figure 12

Assessment of ω on g ( η ) .

Figure 13 
               Assessment of 
                     
                        
                        
                           
                              
                                 R
                              
                              
                                 b
                              
                           
                        
                        {R}_{{\rm{b}}}
                     
                   on 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \theta (\eta )
                     
                  .
Figure 13

Assessment of R b on θ ( η ) .

The influence of Biot number Bi on the temperature profile is shown in Figure 14. As Bi increases, the thermal boundary layer thickness gets wider, which means the thermal Biot number is highly correlated with the heat transference rate. Moreover, owing to the existence of nanoparticles in the fluid, Bi provides support to the transmission of heat into the liquid instead of to the surface. Hence, the temperature profile increases with the increase in Bi . Figure 15 shows the effect of the temperature ratio parameter θ w on the temperature profile. It is found that temperature increases within the boundary layer with the increase of θ w . This result shows that θ w favors the absorption of heat into the liquid. The effect of Brownian constant N b on the thermal profile is shown in Figure 16, which shows that the thickness of the thermal boundary layer increases with high N b values. The movement of particles is crucial in a thermal process. As the value of N b increases, the motion of liquid becomes jumbled and chaotic. The random movement eventually increases the kinetic energy of the particles and leads to an increase in the temperature of the nanoliquid. As shown in Figure 17, the thermophoresis parameter N t increases, it further increases the NF’s temperature. Physically, more thermophoresis force is generated with a higher value of N t , and this force ensures transferring the position of nanoparticles from a hot region to a cool region. Therefore, as N t increases, the motion of particles accelerates, which increases the kinetic energy of molecules and, thus, improves the size of the thermal boundary layer.

Figure 14 
               Assessment of 
                     
                        
                        
                           Bi
                        
                        {\rm{Bi}}
                     
                   on 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \theta (\eta )
                     
                  .
Figure 14

Assessment of Bi on θ ( η ) .

Figure 15 
               Assessment of 
                     
                        
                        
                           
                              
                                 θ
                              
                              
                                 w
                              
                           
                        
                        {\theta }_{{\rm{w}}}
                     
                   on 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \theta (\eta )
                     
                  .
Figure 15

Assessment of θ w on θ ( η ) .

Figure 16 
               Assessment of 
                     
                        
                        
                           Nb
                        
                        {Nb}
                     
                   on 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \theta (\eta )
                     
                  .
Figure 16

Assessment of Nb on θ ( η ) .

Figure 17 
               Assessment of 
                     
                        
                        
                           Nt
                        
                        {Nt}
                     
                   on 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \theta (\eta )
                     
                  .
Figure 17

Assessment of Nt on θ ( η ) .

Figure 18 shows the increment effects of the Brownian constant N b . As the value of N b increases, the concentration profile increases. The reason is, N b greatly helps in the amplification of particles within the fluid. Moreover, N b also increases the random movement of the particles, which somehow affects the increase of the nanoparticle concentration profile. Figure 19 shows that the growth of the thermophoresis parameter N t decreases the concentration of the NF. In this case, the diffusion of the solute is prevented by a higher value of N t , which leads to a decrease in the concentration gradient on the plate. Therefore, the concentration boundary layer thickness shows an expansion behavior along the value of N t .

Figure 18 
               Assessment of 
                     
                        
                        
                           Nb
                        
                        {Nb}
                     
                   on 
                     
                        
                        
                           ϕ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \phi (\eta )
                     
                  .
Figure 18

Assessment of Nb on ϕ ( η ) .

Figure 19 
               Assessment of 
                     
                        
                        
                           Nt
                        
                        {Nt}
                     
                   on 
                     
                        
                        
                           ϕ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \phi (\eta )
                     
                  .
Figure 19

Assessment of Nt on ϕ ( η ) .

The Lewis number Le effect on the microorganism profile is analyzed in Figure 20. It is illustrated that Le increases the density of the microorganisms in the nanoliquid. When there is an increase in the Le , it will lead to an increase in the viscous diffusion rate. The high amount of diffusion rate slows down the rapidity of fluid and thus improves the microorganism profile positively. Figure 21 shows the influence of Peclet number Pe on the microorganism’s profile. As the values of Pe increase, the density of the microorganisms shows a reduction behavior. This means that the Peclet number and the diffusivity of the motile density are inversely related. This indicates that if the value of the Peclet number increases, the diffusivity drops.

Figure 20 
               Assessment of 
                     
                        
                        
                           Le
                        
                        {\rm{Le}}
                     
                   on 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \chi (\eta )
                     
                  .
Figure 20

Assessment of Le on χ ( η ) .

Figure 21 
               Assessment of 
                     
                        
                        
                           Pe
                        
                        {\rm{Pe}}
                     
                   on 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    η
                                 
                                 )
                              
                           
                        
                        \chi (\eta )
                     
                  .
Figure 21

Assessment of Pe on χ ( η ) .

5.1 Primary velocity

Figures 39 show the assessment of primary velocity values.

5.2 Secondary velocity

Figures 1012 show the assessment of secondary velocity values.

5.3 Temperature profile

Figures 1317 show the assessment of temperature profile.

5.4 Concentration profile

Figures 18 and 19 show the assessment of concentration profile.

5.5 Microorganism profile

Figures 20 and 21 show the assessment of microorganism profile.

5.6 Streamlines

Figures 2226 show the streamlines.

Figure 22 
                  Streamlines due to the variation of 
                        
                           
                           
                              A
                           
                           A
                        
                     .
Figure 22

Streamlines due to the variation of A .

Figure 23 
                  Streamlines due to the variation of 
                        
                           
                           
                              K
                           
                           K
                        
                     .
Figure 23

Streamlines due to the variation of K .

Figure 24 
                  Streamlines due to the variation of 
                        
                           
                           
                              ω
                           
                           \omega 
                        
                     .
Figure 24

Streamlines due to the variation of ω .

Figure 25 
                  Streamlines due to the variation of 
                        
                           
                           
                              K
                           
                           K
                        
                     .
Figure 25

Streamlines due to the variation of K .

Figure 26 
                  Streamlines due to the variation of 
                        
                           
                           
                              ω
                           
                           \omega 
                        
                     .
Figure 26

Streamlines due to the variation of ω .

5.7 Isotherms

Figures 2729 show the isotherms.

Figure 27 
                  Isotherms due to the variation of 
                        
                           
                           
                              
                                 
                                    R
                                 
                                 
                                    b
                                 
                              
                           
                           {R}_{{\rm{b}}}
                        
                     .
Figure 27

Isotherms due to the variation of R b .

Figure 28 
                  Isotherms due to the variation of 
                        
                           
                           
                              Bi
                           
                           {\rm{Bi}}
                        
                     .
Figure 28

Isotherms due to the variation of Bi .

Figure 29 
                  Isotherms due to the variation of 
                        
                           
                           
                              
                                 
                                    θ
                                 
                                 
                                    w
                                 
                              
                           
                           {\theta }_{{\rm{w}}}
                        
                     .
Figure 29

Isotherms due to the variation of θ w .

6 Discussion

As shown in Table 1, the buoyancy ratio N r does not show any noticeable changes in the skin friction value. However, the changes are evident for other variables. β , the rapidity slippage A , and the rotation variable ω increase the skin friction value. A fluid with high viscosity favors A to increase the skin friction. The increase of ω strengthens the surface drag force as it decreases the thickness of the boundary layer. However, the skin friction value decreases K , the magnetic field M , the mixed convection parameter λ , and the Rayleigh number N c grow.

Table 1

Skin friction

β A K M ω λ N c N r Cf
0.1 0.1 0.3 0.6 0.2 0.1 0.4 0.3 −3.391850
0.2 −2.913814
0.3 −2.545164
0.1 −3.391850
0.3 −2.054817
0.5 −1.448769
0.1 −2.843097
0.3 −3.391850
0.5 −3.940603
0.2 −3.292077
0.4 −3.341964
0.6 −3.391850
0.1 −3.496612
0.2 −3.391850
0.3 −3.287088
0.1 −3.391850
0.3 −3.422803
0.5 −3.453755
0.2 −3.381374
0.4 −3.391850
0.6 −3.402326
0.1 −3.392326
0.2 −3.392089
0.3 −3.391850

Table 2 shows that the radiation R d , temperature ratio θ w , thermophoresis Nt , Brownian Nb , and Biot Bi parameters increase the Nusselt number. In this case, the increase of Bi , θ w , N b , and N t increase the rate of heat transportation into the fluid, which leads to the improvement of the temperature profile, as shown in Figures 1417, respectively. Logically, the internal energy of particles is intensified by these variables, increasing the thermal energy contained in the molecules.

Table 2

Nusselt number

R d θ w N t N b Bi Nu
0.1 0.2 0.3 0.1 0.4 0.293932
0.3 0.325300
0.5 0.348004
0.1 0.292186
0.2 0.293932
0.3 0.295830
0.1 0.287805
0.3 0.293932
0.5 0.297011
0.1 0.293932
0.3 0.304574
0.5 0.314891
0.2 0.177588
0.4 0.293932
0.6 0.377356

Sherwood number can be defined as the potency of mass transmission over the plate. Table 3 indicates that the Sherwood number is increased with the Brownian constant Nb , decreases with the thermophoresis variable N t , and is barely affected by the Schmidt number Sc .

Table 3

Sherwood number

Sc Nt Nb Sh
0.1 0.1 0.3 −0.058443
0.3 −0.058721
0.5 −0.0589965
0.1 −0.058443
0.2 −0.114285
0.3 −0.168822
0.1 −0.168822
0.2 −0.086581
0.3 −0.058443

Table 4 exhibits the influence of the Lewis number Le , Peclet number Pe , and the concentration difference of the microorganism δ 1 on the microorganism density number. The increase of the Lewis number Le decreases the microorganism density number. The microorganism density number decreases as the Peclet number Pe increases. As the Pe increases, the motion of the microorganism decreases, resulting in the decrease of the diffusion of the microorganism. Pe has a direct relationship with the maximum cell swimming speed and is inversely related to the diffusivity of microorganisms. Therefore, high Pe denotes the low density of microorganisms within the boundary layer. As the microorganism concentration difference δ 1 increases, the rate of the motile microorganism mass transfer decreases. Table 5 shows the comparison of the present skin friction values with those of Rauf et al. [52] for various Casson parameter values.

Table 4

Density numbers of microorganisms

Le Pe δ 1 N n
0.1 0.4 0.1 0.185574
0.2 0.201769
0.3 0.218007
0.2 0.195878
0.4 0.185574
0.6 0.175279
0.1 0.185574
0.3 0.182624
0.5 0.179673
Table 5

Comparison of the present skin friction values with those of Rauf et al. [52] for various β values with M = 0.5 , K = 1.0 , A = 0.0 , and ω = 0.0

β C f [52] C f (present)
0.1 0.38893 0.38893
0.2 0.49585 0.49584
0.3 0.56217 0.56215
2 0.84374 0.84373

7 Conclusions

This theoretical work proposes the three-dimensional flow of Casson nanomaterials under the novel impact of nonlinear thermal radiation and applied magnetic characteristics. This flow is intended to take place in three-dimensional space. In the configuration of the rotating frame, the flow is not taken into consideration. To investigate the potential uses of bioconvection, GMs are utilized in the Casson NF. By adopting the modified Buongiorno thermal nano-model, it is possible to access both the thermophoretic and Brownian mechanisms. It is necessary to have convective boundary conditions to solve the flow problem. It is possible to generate a dimensionless pattern of equations by using suitable variables. Subsequently, semi-analytical simulations are performed using an HAM to obtain the answers to the nonlinear equations. The findings can be summarized as follows.

  1. The velocity profile is affected to increase the effects of N r , β , and ω , while to decrease the velocity profile, the parameters λ , N c , K , and A should be sufficiently high.

  2. The secondary velocity profile can be controlled to decrease with β , K , and ω .

  3. The temperature profile is found to increase with large values of R d , Bi , θ w , N b , and N t .

  4. The concentration profile can be controlled to increase and decrease using the effects of N b and N t , respectively.

  5. While χ can be controlled by controlling Le and Pe to increase and decrease accordingly.

  6. The effects of β , A , ω , and N r parameters will increase the skin friction coefficient while K , M , λ , and N c will decrease the skin friction.

  7. The heat transfer rate can be increased with the increase of R d , θ w , N t , N b , and Bi parameters.

  8. Sc increases with the increase of N b while it decreases with the decrease of N t .

  9. χ can be controlled to increase as Le increases while Pe and δ 1 will be decrease with χ .

The Casson NF flow has attracted a lot of interest in the fields of bioconvection and NF technology because of its special characteristics and prospective uses. Casson NF flow has the following applications and effects in various contexts:

  • Bioconvection enhancement: It has been researched whether Casson NFs, which are suspensions of nanoparticles in a Casson fluid medium, can improve bioconvection processes. Nanoparticles can promote mixing and change flow behavior, which can improve the mass and heat transfer in biological systems. This may have effects on a variety of industries, including biotechnology, environmental engineering, and the generation of biofuels.

  • Biomedical applications: Casson NFs have special characteristics that make them intriguing for biological applications, such as their potential for targeted drug administration and improved heat transfer capabilities. In hyperthermia therapies, where localized heating is utilized to target cancer cells, Casson NFs may be used. Additionally, the exact distribution of drugs to particular parts of the body is made possible by the suspension of therapeutic nanoparticles in Casson fluids.

  • NF technology development: Casson NF research advances the field of NF technology as a whole. In general, NFs have drawn interest as prospective substitutes for traditional heat transfer fluids that offer better thermal characteristics. Our understanding of the complicated fluid dynamics has increased by investigating the behavior and properties of Casson NFs, which also offers insights into the creation of sophisticated NF formulations.

Acknowledgments

The authors extend their appreciation to the Deanship of Scientific Research at King Khalid University for funding this work through large group Research Project under grant number RGP 2/441/44.

  1. Funding information: This work was funded through large group Research Project under grant number RGP 2/441/44 by the Deanship of Scientific Research at King Khalid University.

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors state no conflict of interest.

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Received: 2023-07-01
Revised: 2023-09-21
Accepted: 2023-10-31
Published Online: 2023-12-31

© 2023 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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